CN104015374B - Method for producing frp cylinder and frp cylinder - Google Patents
Method for producing frp cylinder and frp cylinder Download PDFInfo
- Publication number
- CN104015374B CN104015374B CN201410225187.5A CN201410225187A CN104015374B CN 104015374 B CN104015374 B CN 104015374B CN 201410225187 A CN201410225187 A CN 201410225187A CN 104015374 B CN104015374 B CN 104015374B
- Authority
- CN
- China
- Prior art keywords
- prepreg
- frp
- cylinder axis
- axis direction
- wound
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/32—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core on a rotating mould, former or core
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2101/00—Use of unspecified macromolecular compounds as moulding material
- B29K2101/10—Thermosetting resins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
- B29K2105/246—Uncured, e.g. green
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2023/00—Tubular articles
- B29L2023/22—Tubes or pipes, i.e. rigid
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
A method is provided for producing a weight-reduced FRP cylinder which can attain high strength, and also such an FRP cylinder is provided. This FRP cylinder producing method, in which a plurality of prepregs formed by impregnating reinforced fibers with thermosetting resin sheets are wound into a cylinder and thermally cured to be formed as a plurality of FRP layers, includes a simultaneous multilayer winding process in which a torsional rigidity retaining prepreg and a buckling prevention prepreg are continuously wound a plurality of turns with being layered on each other when the plurality of prepregs are wound into a cylinder, wherein the torsional rigidity retaining prepreg includes a layer of fibers oblique to a cylindrical axis direction of the FRP cylinder, and wherein the buckling prevention prepreg includes a layer of fibers orthogonal to the cylindrical axis direction.
Description
The application is Application No. 201080005194.4, and the applying date is on January 14th, 2010, entitled " manufacture
The divisional application of the Chinese patent application of the method and FRP cylinders of FRP cylinders ".
Technical field
The present invention relates to a kind of method of manufacture FPR cylinders, and it is related to a kind of FRP cylinders.
Background technology
In recent years, FRP (fibre reinforced plastics) cylinder is had been used in the middle of various industrial circles.As manufacture FRP cylinders
Method, known method is filament wound method (patent document 1) and prepreg method (patent document 2) in the middle of this area,
In filament wound method, carbon fiber is wrapped in around the heart axle while impregnated of resin, multiple in the middle of prepreg method
Prepreg (each prepreg is made up of the carbon fiber impregnated of thermosetting resin piece) is wound and is thermally cured, to be formed
Multiple FRP layers,.
Prior art literature
Patent document
Patent document 1:The Japanese uncensored patent of Publication No. No.2006-62355.
Patent document 2:The Japanese uncensored patent of Publication No. No.2001-96635.
The content of the invention
The present invention problem to be solved
However, needing the resin more than ormal weight, and the volume of carbon fiber according to the FRP cylinders of filament wound method manufacture
Content has the upper limit, therefore there is a problem of fully meeting the demand that FRP cylinders weight reduces and intensity is improved.
On the other hand, it is according to the characteristic that has of FRP cylinders of prepreg method manufacture:Even if in minimum necessary amounts
Also the volume content of carbon fiber can be increased under resin, so as to the weight that advantageously obtains FRP cylinders simultaneously mitigation and
The raising of intensity.However, being used as the power transmission shaft of automobile (two wheeler) or drive in the FRP cylinders manufactured according to prepreg method
In the case of moving axis, need the FRP cylinders that there is high level intensity (torsional rigidity, roll rigidity and fatigue strength etc.) to support
Resist the power (moment of torsion) being applied on the direction for favouring FRP cylinders on the FRP cylinders and be orthogonal on the direction of FRP cylinders
The power (flexing) being applied on the FRP cylinders, so as to be provided with improved space.
In view of the understanding to the problems referred to above, has been devised by the present invention, and it is an object of the invention to provide a kind of use
Method to manufacture the FRP cylinders of weight saving, the FRP cylinders can reach very high intensity, and the purpose of the present invention is also
It is that this FRP cylinders are provided.
The means of solve problem
As the result being analyzed to traditional FRP cylinders, present inventors have found that:By and large, pass
The FRP cylinders of system be by multiple-turns wound is carried out to prepreg in mutually different machine direction and made by;However, working as
Among the multiple fibers for abutting one another on the inner/outer direction of FRP cylinders on FRP cylinders when applying power, by
In the multiple fibers (fibrage) abutted one another on the inner/outer direction of the FRP cylinders of the prepreg for abutting one another mutually
It is isolated, therefore is difficult the power generation effect for causing to suppress the deformation of these fibers.Although additionally, same prepreg
Base continuous winding multi-turn, but when the prepreg for having been wound up multi-turn has carried out heat cure when, it is difficult to make
Inhibition generation effect in a similar manner must be deformed, this is because abutting one another on the inner/outer direction of FRP cylinders
Machine direction it is mutually the same.Inventor is concluded that these are exactly why traditional FRP cylinders can not represent fully strong
The reason for spending, so as to direct it towards the conception of the present invention.
Specifically, from following viewpoint designing the present invention:Mutually different by winding machine direction
Multiple prepreg and made by the middle of FRP cylinders, the FRP cylinders always include that torsional rigidity keeps prepreg and anti-anti-bend
The prepreg of bent (buckling), the torsional rigidity keeps prepreg to contain the increasing of the longitudinal direction for favouring FRP cylinders
Strong fiber (inclined fiber), this prevents the prepreg of flexing from containing the reinforcing fiber of the longitudinal direction for being orthogonal to FRP cylinders
(orthogonal fiber), therefore, if inclined fiber and orthogonal fiber are with the state continuous winding multi-turn that abuts one another, then can
Make the multiple fibers (fibrage) for extending in one direction and extend in the other directions including other fibers (fibrage)
The circle of stacking two or more multi-turn are adjacent on portion/outside direction.Therefore, interior fibrage and outer fibre layer prevent mutually it from deforming, from
And intensity can be improved.In other words, if orthogonal fiber (inclined fiber) and inclined fiber (orthogonal fiber) be laminated and
The circle of winding two or more multi-turn (to form simultaneously wound multilayer/many windings layer/mono- group winding layer), wherein orthogonal fiber
(inclined fiber) is clipped between inclined fiber (orthogonal fiber), then can improve the intensity of FRP cylinders, this is because, Ke Yishe
Expect, when outer masterpiece uses FRP cylinders, the fibrage for adjoining cooperate with each other ground resistance to deformation.
Method for manufacturing FRP cylinders of the invention is characterised by, multiple prepreg are wound up as into cylinder
And carry out heat cure, to form multiple FRP layers, the prepreg by by reinforcing fiber impregnated of thermosetting resin piece shape
Into, methods described includes the multi-lay winding process for carrying out simultaneously, wherein when the plurality of prepreg is wound up as cylinder,
Torsional rigidity keeps prepreg and prevents the prepreg of flexing to be continuously wound multi-turn while stacking mutually, its
Described in torsional rigidity keep prepreg include favour the FRP cylinders cylinder axis direction fibrage, and its
In, it is described to prevent the prepreg of flexing from including being orthogonal to the fibrage in the cylinder axis direction.
By this configuration, the FRP cylinders of the high intensity relative to torsional direction and buckling direction are obtained in that, this is adapted to
In the power transmission shaft as automobile and drive shaft.
Described while during the multi-lay winding for carrying out, the torsional rigidity keeps prepreg and described prevents flexing
Prepreg prepreg is kept by bending stiffness and multi-turn has been continuously wound, the bending stiffness keeps prepreg
Including the fibrage parallel to the cylinder axis direction, and the bending stiffness keeps prepreg to be further layered in the torsion
Turn rigidity to keep in prepreg and the prepreg for preventing flexing.
By this configuration, to be obtained in that and there is intensity and relative to torsional direction and flexing side relative to bending direction
To the FRP cylinders with intensity, and the FRP drum fits are in the stabiliser bar as automobile or anti-roll lever.
It is desirable that described while the multi-lay winding process for carrying out is performed at least twice.It is desirable that in winding contrary mutually
To described while the multi-lay winding process for carrying out is performed at least twice on direction.
It is desirable that described while the multi-lay winding process for carrying out is using separate sheet (for example, PTFE films or PFA films)
Carry out, the separate sheet is clipped between the prepreg adjoined under laminated arrangement that (torsional rigidity keeps prepreg and preventing
The prepreg of flexing, torsional rigidity keep prepreg and bending stiffness to keep prepreg or prevent the preimpregnation of flexing
Material base and bending stiffness keep prepreg), and during the operation of the multi-lay winding for the carrying out process simultaneously, by described point
Remove from piece.
It is desirable that described while each the prepreg (torsional rigidity being wound during the multi-lay winding for carrying out
Keep prepreg and prevent the prepreg of flexing, and bending stiffness keeps prepreg) all in the cylinder axis side
There is upwards identical length, and on the cylinder axis direction, whole length of multiple prepreg in the FRP cylinders
It is stacked mutually on degree.For the FRP cylinders with traditional structure, typically, will be used for preventing the cross section of FRP cylinders from bending
The bent prepreg of flexing that prevents marginally is inserted in the middle of a part for FRP cylinders on cylinder axis direction, therefore, can
Can occur such as this prevent the prepreg of flexing from cannot easily insert and product occur distort problem.In the present invention
It is central, by being examined closely again to this conventional well known technology general knowledge, can pass through cause prevent flexing prepreg and
Torsional rigidity keeps prepreg (bending stiffness holding prepreg) to have equal length on cylinder axis direction, and makes
These prepreg continuous winding multi-turns, so as to solve such as this prevent the prepreg of flexing from cannot easily insert and
There is the problem for distorting in product.
FRP cylinders of the invention are characterised by that the FRP cylinders have multiple prepreg, the prepreg
By the way that reinforcing fiber is formed impregnated of thermosetting resin piece, and the prepreg is wound up as cylinder and has carried out thermosetting
Change, to be formed as multiple FRP layers, wherein the plurality of FRP layers include simultaneously wound multilayer, the multilayer is by one group of prepreg
Configuration is formed, and one group of prepreg continuous winding multi-turn is simultaneously thermally cured, wherein one group of prepreg includes mutual layer
Folded torsional rigidity keeps prepreg and prevents the prepreg of flexing, wherein the torsional rigidity keeps prepreg to include
The fibrage in the cylinder axis direction of the FRP cylinders, and the wherein described prepreg for preventing flexing are favoured including just
Meet at the fibrage in the cylinder axis direction.
From for practice so that the torsional rigidity keeps prepreg to include a pair of biasing prepreg, and the biasing is pre-
The filament fiber direction of leaching material base is with ± α degree (0<α<90) angle and favour the cylinder axis direction, and cause institute
Stating prevents the prepreg of flexing from including hoop prepreg, and the filament fiber direction of the hoop prepreg is orthogonal to the circle
Cylinder axis direction.In this case, it is desirable that it is the pair of biasing prepreg filament fiber direction with ± 30 degree, ±
45 degree or ± 60 degree of angle favours the cylinder axis direction.
One group of prepreg can also include that being layered in the torsional rigidity keeps prepreg and the anti-anti-bend
Bending stiffness in bent prepreg keeps prepreg, and the bending stiffness keeps prepreg to have parallel to the cylinder
The fibrage of axis direction.In this case, from for practice so that it is 0 degree of preimpregnation that the bending stiffness keeps prepreg
Material base, the filament fiber of 0 degree of prepreg is oriented parallel to the cylinder axis direction.
Alternately, the torsional rigidity can be caused to keep prepreg to include that plain weave fabric prepreg, three axles are compiled
Woven fabric prepreg or four axle braided fabric prepreg, wherein the plain weave fabric prepreg is by impregnated of thermosetting tree
The plain weave fabric of fat piece is constituted, and the plain weave fabric prepreg includes favouring the fibrage in the cylinder axis direction,
Wherein described three axles braided fabric prepreg is made up of the three axle braided fabrics impregnated of thermosetting resin piece, and the three axles braiding
Fabric prepreg material base includes favouring the fibrage in the cylinder axis direction, and wherein described four axles braided fabric prepreg
Base is made up of the four axle braided fabrics impregnated of thermosetting resin piece, and the four axles braided fabric prepreg is described including favouring
The fibrage in cylinder axis direction.Additionally, the prepreg for preventing flexing can include plain weave fabric prepreg or
Four axle braided fabric prepreg, wherein the plain weave fabric prepreg is by the plain weave fabric structure impregnated of thermosetting resin piece
Into, and the plain weave fabric prepreg includes being orthogonal to the fibrage in the cylinder axis direction, and wherein described four axle
Braided fabric prepreg is made up of the four axle braided fabrics impregnated of thermosetting resin piece, and the four axles braided fabric prepreg
Including the fibrage for being orthogonal to the cylinder axis direction.
It is desirable that one group of prepreg continuous winding three enclose or more multi-turn and be wound up as cylinder.
It is desirable that the plurality of FRP layers include multilayer simultaneously wound described at least two.In this case, respectively
At least two groups prepreg for forming the simultaneously wound multilayer are alternately wound with winding direction contrary mutually.
It is desirable that the plurality of FRP layers include the outermost layer for preventing explosion layer to be used as the FRP layers, this prevents the layer that bursts
It is made up of hoop prepreg, the filament fiber direction of the hoop prepreg is orthogonal to the cylinder axis direction.
It is desirable that each prepreg of one group of prepreg (torsional rigidity keeps prepreg and prevents flexing
Prepreg, and bending stiffness keep prepreg) on the cylinder axis direction have identical length, and
On the cylinder axis direction, multiple prepreg of one group of prepreg are mutual in the whole length of the FRP cylinders
It is mutually stacked.
Invention effect
According to the present invention, because methods described includes the multi-lay winding process while carrying out, wherein when multiple prepreg
When being wound up as cylinder, torsional rigidity keeps prepreg and prevents the prepreg of flexing from being connected while stacking mutually
Multi-turn is wound with continuously, wherein the torsional rigidity keeps prepreg to include favouring the cylinder axis side of the FRP cylinders
To fibrage, it is and wherein, described to prevent the prepreg of flexing from including being orthogonal to the fibrage in the cylinder axis direction,
It is obtained in that the FRP cylinders of the high intensity relative to torsional direction and buckling direction.Furthermore it is possible to realize the weight of FRP cylinders
Mitigation is improved with intensity, this is because can pass through to reduce that the torsional rigidity for constituting one group of prepreg holding be included in advance
Soak material base and prevent the amount of resin in the prepreg of flexing, so as to improve the amount of reinforcing fiber.
Description of the drawings
Fig. 1 is to show the multi-lay winding carried out while being included in FRP cylinders with regard to first embodiment of the invention
The view of layer;
Fig. 2 is regarding for the structure of one group of prepreg of the multi-lay winding layer carried out while showing to include shown in Fig. 1
Figure;
Fig. 3 is the view of the structure for showing the prepreg for preventing bursting;
Fig. 4 is the view of the structure for showing FRP cylinders, and the FRP cylinders in cylinder mode by being wound up as the pre- of FRP layers
Leaching material base carries out heat cure and makes;
The view of the multi-lay winding layer that Fig. 5 is carried out while being and show to be included in FRP cylinders, the FRP cylinders are by profit
The plurality of layer is wound with the separate sheet being clipped between multiple layers and is made;
Fig. 6 is to show the multi-lay winding carried out while being included in FRP cylinders with regard to second embodiment of the invention
The view of layer;
Fig. 7 is to show the multi-lay winding carried out while being included in FRP cylinders with regard to third embodiment of the invention
The view of layer;
Fig. 8 is regarding for the structure of one group of prepreg of the multi-lay winding layer carried out while showing to include shown in Fig. 7
Figure;
Fig. 9 shows the multi-lay winding layer carried out while being included in FRP cylinders with regard to four embodiment of the invention
View;
Figure 10 is regarding for the structure of one group of prepreg of the multi-lay winding layer carried out while showing to include shown in Fig. 9
Figure;
Figure 11 is shown in the case that the number of turns of one group of prepreg changes, while the multi-lay winding for carrying out
The view of layer;
Figure 12 is to show the multi-lay winding carried out while being included in FRP cylinders with regard to fifth embodiment of the invention
The view of layer;
Figure 13 is the structure of one group of prepreg of the multi-lay winding layer carried out while showing to include shown in Figure 12
View;
Figure 14 is to show the multi-lay winding carried out while being included in FRP cylinders with regard to sixth embodiment of the invention
The view of layer;
Figure 15 is the structure of one group of prepreg of the multi-lay winding layer carried out while showing to include shown in Figure 14
View;
Figure 16 is the view of the structure for showing the plain weave fabric prepreg that prepreg is kept as torsional rigidity;
Figure 17 is the first of the structure for showing the three axle braided fabric prepreg that prepreg is kept as torsional rigidity
View;
Figure 18 is the second of the structure for showing the three axle braided fabric prepreg that prepreg is kept as torsional rigidity
View;
Figure 19 is to show the four axle braided fabrics for keeping prepreg as torsional rigidity or preventing the prepreg of flexing
The view of the structure of prepreg;
Figure 20 is the view for showing the structure as the plain weave fabric for preventing flexing layer;
Figure 21 be for being displayed in the example of practice in, the prepreg in each the FRP cylinder manufactured for test
Multi-lay winding structure the first chart;
Figure 22 be for being displayed in the example of practice in, the prepreg in each the FRP cylinder manufactured for test
Multi-lay winding structure the second chart;
Figure 23 be for being displayed in the example of practice in, the prepreg in each the FRP cylinder manufactured for test
Multi-lay winding structure the 3rd chart.
Specific embodiment
(the first embodiment)
Fig. 1 is to show winding while being included in FRP cylinders 100 (Fig. 4) with regard to first embodiment of the invention
The view of multilayer 10.The FRP cylinders 100 are by the way that multiple prepreg are wound up as into cylinder and to multiple preimpregnation of such winding
Material base carry out heat cure and made by, so as to constitute multiple FRP layers, wherein each prepreg is by by thermosetting resin piece
Made by impregnated of reinforcing fiber.In FIG, it is only many to being included in this in order that the present invention is easier to understand
The multilayer 10 wound while in individual FRP layers is shown.
The simultaneously wound multilayer 10 has torsional rigidity retaining layer 20 and prevents the layer 30 of flexing, and the torsional rigidity keeps
Layer 20 has certain intensity come (hereinafter referred to as " cylinder axis the direction ") Jing on the axis direction for favouring FRP cylinders 100
It is described to prevent the layer 30 of flexing that there is certain intensity to be orthogonal to cylinder by the power (moment of torsion) being applied on FRP cylinders 100
Undergo the power (flexing) being applied on FRP cylinders 100 on axis direction.Torsional rigidity retaining layer 20 by a pair of bias layer 20A and
20B is constituted.
More specifically, simultaneously wound multilayer 10 is formed by one group of configuration of prepreg 1, one group of prepreg
1 is kept prepreg 2 by torsional rigidity and prevents the prepreg 3 of flexing to constitute, and torsional rigidity keeps the He of prepreg 2
Prevent the prepreg 3 of flexing as shown in Figure 2 according to being sequentially laminated from that of bottom (inner side), and one group
Prepreg 1 continuous winding multi-turn is simultaneously thermally cured, and wherein torsional rigidity keeps prepreg 2 to include favouring cylinder axis
The fibrage in direction, preventing the prepreg 3 of flexing includes being orthogonal to the fibrage in cylinder axis direction.Fig. 2 shows torsion
Rigidity keeps prepreg 2 and prevents the state of one group of prepreg 1 before the mutual stacking of prepreg 3 of flexing, with right
The torsional rigidity for constituting one group of prepreg 1 keeps prepreg 2 and prevents the fiber side of each of the prepreg 3 of flexing
To being shown.It is noted that previous-next (interior-outer) position relationship between multiple prepreg is flexibility and changeability;Can pass through
Prepreg 2 is kept sequentially to carry out layer according to from that of bottom (inner side) prepreg 3 and torsional rigidity that prevent flexing
Fold to manufacture one group of prepreg 1.
Torsional rigidity keeps prepreg 2 to become torsional rigidity retaining layer 20 by heat cure;In the embodiment
Central, torsional rigidity keeps prepreg 2 to be made up of a pair of biasing prepreg 2A and 2B.The filament of this pair of biasing prepreg
Machine direction is with ± α degree (0<α<90) angle and favour cylinder axis direction.Angle [alpha] be, for example, ± 30 degree, ± 45 degree or
± 60 degree.The prepreg 3 for preventing flexing becomes to prevent the layer 30 of flexing by heat cure, and this prevents the prepreg of flexing
Base 3 is hoop prepreg, and the filament fiber direction of the hoop prepreg is orthogonal to cylinder axis direction.
The width W settings of one group of prepreg 1 (torsional rigidity keeps prepreg 2 and prevents the prepreg 3 of flexing)
To be wound around about three times of the girth of one group of prepreg 1 for cylinder, and one group of prepreg 1 being capable of continuous winding three
Enclose and be wound up as cylinder.Because one group of prepreg 1 is made up of three prepreg:A pair of biasing prepreg 2A and 2B and
Hoop prepreg 3, therefore cylinder is wound up as by the way that one group of continuous winding three of prepreg 1 is enclosed, the quantity of lamination is altogether
It is changed into nine.One group of prepreg 1 (torsional rigidity keeps prepreg 2 and prevents the prepreg 3 of flexing) is in cylinder axis side
There is upwards identical (equivalent) length, and on cylinder axis direction, torsional rigidity keeps prepreg 2 and anti-anti-bend
Bent prepreg 3 is stacked mutually in the whole length of one group of prepreg 1.Notice that length L corresponds to FRP cylinders 100
Length, and length L is designed according to the purposes of FRP cylinders 100.
Various prepreg are wrapped in the inner side or outside of one group of prepreg 1 according to the purposes of FRP cylinders 100,
And these various prepreg become the FRP layers different from simultaneously wound multilayer 10 by heat cure.For example, it is preferable
Ground, the outermost layer of multiple FRP layers of FRP cylinders is constituted prevents the layer that bursts, and it is by preventing explosion that this prevents explosion layer
Prepreg 7 (hoop prepreg) carry out heat cure and made by, the direction of its filament fiber is orthogonal to cylinder axis direction
(Fig. 3).This prevents explosion layer from preventing FRP cylinders 100 to burst when compression is buckled, and enhances FRP cylinders
100 relative to buckling direction intensity.Prevent the width W ' of the prepreg 7 for bursting is carried out according to its number of turns (lamination quantity)
Design.Further, it is also possible to bending stress retaining layer is installed on any a layer of multiple FRP layers (prevents what axis direction from compressing
Layer), the bending stress retaining layer is the filament of 0 degree of prepreg made by by carrying out heat cure to 0 degree of prepreg
Machine direction is parallel to cylinder axis direction.
In addition to carbon fiber, alumina fibre, aramid fibre, Tai Lunnuo (Tyranno) fiber, amorphous fibre
Dimension, glass fibre etc. can act as being included in the reinforcing fiber in the middle of various prepreg, and the prepreg includes above-mentioned
Torsional rigidity keep prepreg 2, prevent flexing prepreg 3 and prevent burst (the 0 degree of prepreg of prepreg 7
Base).In other words, wire type is not fundamentally limited to particular type.
Keep prepreg 2 (a pair of biasing prepreg 2A and 2B), prevent (hoop) of flexing in such as torsional rigidity
In the case that the unidirectional fibre of prepreg 3 or (hoop) prepreg 7 for preventing from bursting strengthens prepreg (that is, carefully
The direction of silk fiber arranges in one direction), wire thickness is desirably less than 24K (1K=1,000 filament).If silk thread
Thickness then possibly cannot guarantee uniform fabric property more than 24K;Additionally, surrounding heart axle during manufacture to wind prepreg
The machinability of base may be deteriorated.
This resin for strengthening fabric dipping can be arbitrary type from for essence.It is, for example possible to use asphalt mixtures modified by epoxy resin
Fat, unsaturated polyester resin, phenolic resin, vinyl ester resin, polyether-ether-ketone (peek) resin, polyimide resin etc..
It is desirable that the weight of each prepreg is less than 300g/m2, more desirably less than 250g/m2.If weight surpasses
Cross 300g/m2, then prepreg become blocked up, so as to be difficult be wound around heart axle during manufacture.It is included in each pre-
Amount of resin in the middle of leaching material base is ideally in the range of 45 20 the percent to percent of weight ratio;It is more preferable
Ground is 40 25 the percent to percent of weight ratio.If the weight content of resin is below 20 percent,
Then the axle with sufficient intensity possibly cannot be produced due to the too resin of a small amount of.If the weight content of resin exceedes percentage
45, then compared with the cylinder with identical weight, torsional rigidity may deteriorate.
Placing as discussed above the FRP cylinders 100 of configuration can improve intensity relative to torsional direction and buckling direction,
This is because simultaneously wound multilayer 10 is manufactured between the multiple FRP layers for being included in the main body including FRP cylinders 100, should
Simultaneously wound multilayer 10 is that (it keeps prepreg 2 and anti-anti-bend by the torsional rigidity being laminated mutually by one group of prepreg 1
Bent prepreg 3 is constituted) continuous winding multi-turn and carry out heat cure (wherein torsional rigidity keeps prepreg 2 to include inclining
In the fibrage in cylinder axis direction, preventing the prepreg 3 of flexing includes being orthogonal to the fibrage in cylinder axis direction) configuration
.FRP cylinders 100 with this structure are adapted for use as the power transmission shaft or drive shaft of automobile.
(that is, a pair of biasing prepreg 2A and 2B and hoop prepreg 3) is grand further, since three prepreg
It is laminated and is then wound while is considered as single prepreg base (one group of prepreg 1) in sight, so with
The situation that the material of identical weight independently winds is compared, and prevents being presented as flexing effect can be while realizing FRP cylinders 100
The mitigation of weight and the raising of intensity.
Next, the method for manufacture FRP cylinders 100 described below, the FRP cylinders 100 are carried out as described above
Configuration.Manufacture method described below is only example;Can enter in the case of without departing from the spirit and scope of the present invention
The various changes of row.
(including one group of prepreg 1, each prepreg in one group of prepreg 1 is by soaking for multiple prepreg
The carbon fiber of stain thermosetting resin piece is made) around the heart axle (hereinafter referred to as " heart axle ") of shaft-like (column) made by metal material
The periphery of M is wound.That is, multiple prepreg are wrapped in around the periphery of heart axle M, with the layer for carrying out multilayer thereon
Folded, its lamination order is formed from the prepreg of the most interior FRP layers of FRP cylinders 100 to the outermost FRP for forming FRP cylinders 100
The prepreg of layer.It is desirable that this many layer operations are performed under predetermined pre- Warm status, such that it is able to come around heart axle M
Winding prepreg, its canoe causes the prepreg adjoined closely to be laminated mutually.
When completing the winding of all prepreg around heart axle M, by contraction band or its class under tension force
It is wrapped in prepreg like thing, and prepreg carries out heat cure by heater (such as baking oven), wherein outside
Pressure acts on prepreg.It is desirable that the heating and solidification process are carried out in a vacuum (for example, in the middle of pressure cooker).Cause
This, the multiple prepreg being wrapped in around heart axle M are thermally cured all-in-one-piece FRP cylinders.That is, one group of quilt of prepreg 1
Heat cure and become simultaneously wound multilayer 10.
Subsequently, FRP cylinders 100 (Fig. 4) are completed by the way that heart axle M is pulled out, the FRP cylinders 100 have internal diameter φ, outer
Footpath Ф and length L, internal diameter φ is corresponding to the external diameter of heart axle M, and external diameter Ф adds the thickness of multiple FRP layers corresponding to internal diameter φ, long
Length of the degree L corresponding to prepreg.
According to the method for manufacturing FRP cylinders of the present embodiment, to one group of continuous winding multi-turn (its of prepreg 1
Middle torsional rigidity keeps prepreg 2 to include favouring the fibrage in cylinder axis direction, and prevents the prepreg 3 of flexing
Fibrage including cylinder axis direction is orthogonal to) process be included in by multiple prepreg be wound up as cylinder process work as
In, one group of prepreg 1 by the torsional rigidity that is laminated mutually keep prepreg 2 (a pair of biasing prepreg 2A and 2B) and
The prepreg (hoop prepreg) 3 for preventing flexing is constituted.In other words, the multi-lay winding process that this is carried out simultaneously is will be multiple
Prepreg (three prepreg:Torsional rigidity keeps a pair of biasing prepreg 2A and 2B of prepreg 2, and prevents
The prepreg 3 of flexing) process of multi-turn is continuously wound around heart axle M, as the plurality of prepreg is single pre-
Leaching material base (one group of prepreg 1).
It is desirable that while the multi-lay winding process for carrying out is carried out by multiple separate sheets, these separate sheets are clipped in stacking
Between adjacent courses under state (separate sheet winding).Fig. 5 shows this embodiment.In the middle of the embodiment, while entering
What capable multi-lay winding process was carried out by separate sheet P1 and separate sheet P2, separate sheet P1 is clipped in torsional rigidity and keeps preimpregnation
Material base 2 (torsional rigidity retaining layer 20) and prevent flexing prepreg 3 (preventing the layer 30 of flexing) between, separate sheet P2 folder
Bias between prepreg 2A and 2B (a pair of bias layers 20A and 20B) at a pair.Can be used using fluororesin (coating) film
Make separate sheet P1 and P2, for example for example, PTFE films or PFA films.
Wound according to above-mentioned separate sheet, one group of prepreg 1 can equably wind;Additionally, greatly improving FRP circles
The formability of cylinder 100, and its internal structure and external structure can be made splendid.Therefore, it is not necessary to FRP cylinders
100 surface is polished so that it becomes smooth by post processing, and also surface need not be painted to improve FRP circles
The outward appearance on the surface of cylinder 100.(separate sheet is succeedingly removed during the multi-lay winding process that separate sheet P1 and P2 are carried out at the same time
Remove process).Process is removed for the ease of the separate sheet, the width of each separate sheet P1 and P2 is set greater than and is longer than
The width W of one group of prepreg 10.Additionally, on the position that winding starts, each separate sheet P1 and P2 are slightly recessed one
In the middle of group prepreg 1 (simultaneously wound multilayer 10).
(the second embodiment)
Fig. 6 is to show the multilayer 10 wound while being included in FRP cylinders with regard to second embodiment of the invention
View.In the middle of the embodiment, torsional rigidity keeps prepreg 2 and prevents the winding start bit of the prepreg 3 of flexing
Put be formed it is mutually different, so as to simultaneously wound multilayer 10 torsional rigidity retaining layer 20 and prevent the layer 30 of flexing mutual
Skew (skew winding).More specifically, prepreg 2 (a pair of biasing prepreg 2A and 2B) has been kept from torsional stiffnesses
Jing is wound for point (winding starting position) place of cylinder, and torsional rigidity keeps prepreg 2 and prevents the prepreg 3 of flexing
The circle of ground continuous winding two is stacked mutually.The skew winding can strengthen anti-anti-bend in the outer layer for receiving higher shear stress
Bent effect such that it is able to so that FRP cylinders have higher intensity.
Torsional rigidity keeps prepreg 2 and prevents the drift rate between the winding starting position of the prepreg 3 of flexing
(side-play amount) can change according to the purposes of FRP cylinders.Additionally, the FRP cylinders of the second embodiment can be with real with first
Apply the FRP cylinders similar mode of scheme to be manufactured.
Although torsional rigidity keeps prepreg 2 and prevents the prepreg 3 of flexing to be mutually shifted in figure 6, can
So that a pair of biasing prepreg 2A and 2B are mutually shifted.For example, the winding starting position of three below prepreg can be with
Be arranged to it is mutually different, that is, a pair of biasing prepreg 2A and 2B and prevent the prepreg 3 of flexing.Additionally, this three
The stacking order of individual prepreg is not restricted to as shown in Fig. 6;For example, can cause to prevent flexing prepreg and
A pair of biasing prepreg are laminated with the order started from internal layer side.
(the 3rd embodiment)
Fig. 7 is to show the multilayer 10 wound while being included in FRP cylinders with regard to third embodiment of the invention
View.The FRP cylinders of the embodiment have two simultaneously wound multilayers 10 and 40, and it is respectively by two groups of prepreg 1 and 4
It is fabricated by.One group of prepreg 4 has the identical structure of one group of prepreg 1 with the first embodiment, and this group
Prepreg 4 is by the way that the torsional rigidity being made up of a pair of biasing prepreg 5A and 5B is kept into prepreg 5 and anti-anti-bend
Bent (hoop) prepreg 6 mutually stacking and made by (Fig. 8).By each of the multilayer 10 and 40 simultaneously wound to two groups
Person's continuous winding three is enclosed, and the total number of lamination is changed into 18.
Include two simultaneously wound multilayers 10 and 40, energy in multiple FRP layers of FRP cylinders by causing FRP cylinders
The enough intensity for further increasing FRP cylinders.Can suitably be changed according to the purposes of FRP cylinders and be included in FRP cylinders
The quantity of the multilayer wound while in multiple FRP layers, for example, FRP cylinders can be manufactured into the multiple FRP in FRP cylinders
Layer includes three or more simultaneously wound multilayers.In this case, used corresponding to simultaneously wound multilayer
Multigroup prepreg of quantity.
Although the FRP cylinders of the present embodiment can be carried out in the way of the FRP cylinders similar to the first embodiment
Manufacture, but it is desirable that the multi-lay winding process carried out while for one group of prepreg 1 and for one group of prepreg 4
While the multi-lay winding process that carries out (rightabout) alternately on mutually opposite winding direction.It is shown in the figure 7
Example in the middle of, when one group of prepreg 1 in the clockwise direction (for Fig. 7 from left to right) rotation heart axle M around
After winding, one group of prepreg 4 is carried out around the heart axle M of rotation in the counterclockwise direction (for Fig. 7 from right to left)
Winding.This enhances in a circumferential direction the uniformity of the FRP layers of FRP cylinders, and enhances the intensity of FRP cylinders and its outer
See.
(the 4th embodiment)
Fig. 9 is to show the multilayer 70 wound while being included in FRP cylinders with regard to four embodiment of the invention
View.Represented by identical reference number with element as the element class of the first embodiment, and it is right by omitting
The description of these elements.
In addition to torsional rigidity retaining layer 20 with the layer 30 for preventing flexing, it is firm that simultaneously wound multilayer 70 has been additionally provided with bending
Degree retaining layer 80, the intensity that the bending stiffness retaining layer 80 has can undergo to be applied on parallel to cylinder axis direction
Power (moment of flexure) on FRP cylinders.
That is, simultaneously wound multilayer 70 is formed by one group of configuration of prepreg 1 ', and one group of prepreg 1 ' is by such as scheming
The bending stiffness for starting sequentially to be laminated from bottom (inner side) as shown in 10 keeps prepreg 9, torsional rigidity to keep preimpregnation
Material base 2 and prevent the prepreg 3 of flexing to constitute, and one group of prepreg 1 ' by continuous winding multi-turn and by thermosetting
Change, wherein the bending stiffness keeps prepreg 9 to include the fibrage parallel to cylinder axis direction, the torsional rigidity keeps pre-
Leaching material base 2 includes favouring the fibrage in cylinder axis direction, and this prevents the prepreg 3 of flexing from including being orthogonal to cylinder
The fibrage of axis direction.Bending stiffness keeps prepreg 9 to become bending stiffness retaining layer 80 by heat cure;At this
In the middle of embodiment, it is 0 degree of prepreg that bending stiffness keeps prepreg 9, and its filament fiber is oriented parallel to cylinder axis
Direction.Figure 10 shows that the bending stiffness for constituting one group of prepreg 1 ' keeps prepreg 9, torsional rigidity to keep prepreg
2 and prevent flexing prepreg 3 it is stacked together before state, so as to show each of these prepreg 9,2 and 3
The filament fiber direction of person.
(bending stiffness keeps prepreg 9, torsional rigidity to keep prepreg 2 and prevent to the width W of one group of prepreg 1 '
The bent prepreg 3 of anti-bend) it is configured to when these prepreg are wound up as cylinder approx slightly larger than these preimpregnation
Three times of the girth of material base, so as to one group of prepreg 1 ' can continuous winding three enclose and be wound up as cylinder.Due to one group of preimpregnation
Material base 1 ' is made up of following four prepreg:Bending stiffness keep prepreg 9, a pair of biasing prepreg 2A and 2B and
Hoop prepreg 3, therefore, by the way that one group of continuous winding of prepreg 1 ' three is enclosed, then the quantity of lamination is changed into 12 altogether.
Continuous winding is not limited to three circles for the number of turns of one group of prepreg 1 ' of cylinder, and can suitably carry out
Change.For example, as shown in figure 11, cylinder is wound up as by the way that one group of continuous winding of prepreg 1 ' five is enclosed, then the number of lamination
Amount is changed into 20 altogether.
According to the FRP circles that the multilayer 70 for winding while configure as mentioned above is provided with multiple FRP layers of FRP cylinders
Cylinder, the FRP cylinders are obtained in that relative to the intensity of bending direction and relative to torsional direction and the intensity of buckling direction.Tool
The FRP cylinders 100 for having these characteristics are suitable as the stabiliser bar or anti-roll lever of automobile.
The multilayer 70 wound while the present embodiment can also be with the mode system similar with the first embodiment
Make.Furthermore, it is possible to arrange two or more simultaneously wound multilayers 70;In this case, it is desirable that these prepreg
Group 1 ' alternately winds on mutually opposite winding direction.
(the 5th embodiment)
Figure 12 is to show the multilayer 90 wound while being included in FRP cylinders with regard to fifth embodiment of the invention
View.Simultaneously wound multilayer 90 is provided with the first bias layer 20A, bending stiffness retaining layer 80, the second bias layer 20B and anti-anti-bend
Bent layer 30, the intensity that first bias layer 20A has can undergo to be applied on the direction for favouring cylinder axis direction
Power (moment of torsion) on FRP cylinders;The intensity that the bending stiffness retaining layer 80 has can undergo parallel to cylinder axis side
To direction on be applied to power (moment of flexure) on FRP cylinders;The intensity that second bias layer 20B has can undergo favouring circle
The power (moment of torsion) being applied on the direction of cylinder axis direction on FRP cylinders;The intensity that the layer 30 for preventing flexing has can
Undergo be orthogonal on the direction in cylinder axis direction the power (flexing) that is applied on FRP cylinders.
More specifically, simultaneously wound multilayer 90 is by one group of prepreg 1 " configuration form, one group of prepreg
1 " by as shown in Figure 13 from bottom (inner side) be sequentially laminated biasing prepreg 2A, bending stiffness keep preimpregnation
Material base 9, biasing and prevent the prepreg 3 of flexing to constitute at prepreg 2B, and one group of prepreg 1 " by continuous winding
Multi-turn is simultaneously thermally cured, wherein the filament fiber direction of biasing prepreg 2A is with the angles of+45 degree and cylinder axis directions
Incline, bending stiffness keeps prepreg 9 to include the fibrage parallel to cylinder axis direction, biases the filament of prepreg 2B
Machine direction is inclined with the angle of -45 degree and cylinder axis direction, and this prevents the prepreg 3 of flexing from including being orthogonal to circle
The fibrage of cylinder axis direction.Figure 13 shows that biasing prepreg 2A, bending stiffness keep prepreg 9, biasing prepreg
State before base 2B is stacked together with the prepreg 3 for preventing flexing, so as to show one group of prepreg 1 is constituted "
These prepreg 2A, 9, the filament fiber direction of each of 2B and 3.
(biasing prepreg 2A, bending stiffness keep prepreg 9, biasing prepreg to the width W of one group of prepreg 1 "
Base 2B and the prepreg 3 for preventing flexing) it is configured to approx be more than this when these prepreg are wound up as cylinder
Three times of the girth of a little prepreg, also, by by one group of prepreg 1 " continuous winding five is enclosed, then the quantity of lamination is altogether
It is changed into 20.
According to the FRP circles that the multilayer 90 for winding while configure as mentioned above is provided with multiple FRP layers of FRP cylinders
Cylinder, (biasing prepreg 2A and bending stiffness keep prepreg 9, bending stiffness to keep the and of prepreg 9 to adjoin prepreg
Biasing prepreg 2B and biasing prepreg 2B and prevent the prepreg 3 of flexing) between angle difference be all 45
Degree, which reduces distortion deviation between layers, such that it is able to prevent stripping/peeling between layers.
The multilayer 90 wound while the present embodiment can also be with the mode system similar with the first embodiment
Make.Furthermore, it is possible to arrange two or more simultaneously wound multilayers 90;In this case, it is desirable that these prepreg
Group 1 " alternately winds on mutually opposite winding direction.
(the 6th embodiment)
Figure 14 is to show regarding for the multilayer wound while being included in FRP cylinders with regard to sixth embodiment of the invention
Figure.The FRP cylinders of the embodiment have two simultaneously wound multilayers 95 and 96, they respectively by two groups of prepreg 1X and
1Y configurations are formed.
As shown in figure 15, simultaneously wound multilayer 95 is formed by one group of prepreg 1X configuration, one group of prepreg
1X by as shown in Figure 15 from bottom (inner side) be sequentially laminated prevent flexing prepreg 3, biasing prepreg
Base 2A, bending stiffness keep prepreg 9 and biasing prepreg 2B to constitute, and one group of prepreg 1X continuous winding is more
Enclose and be thermally cured, wherein prevent the prepreg 3 of flexing to include being orthogonal to the fibrage in cylinder axis direction, bias prepreg
The filament fiber direction of base 2A favours cylinder axis direction with the angle of+45 degree, and it is flat that bending stiffness keeps prepreg 9 to have
Row favours cylinder in the fibrage in cylinder axis direction, the filament fiber direction for biasing prepreg 2B with the angle of -45 degree
Axis direction.On the other hand, simultaneously wound multilayer 96 is formed by one group of prepreg 1Y configuration, one group of prepreg 1Y
Biasing prepreg 2B, bending stiffness holding prepreg 9, the biasing prepreg being sequentially laminated by from bottom (inner side)
2A and prevent the prepreg 3 of flexing to constitute, and one group of prepreg 1Y continuous winding multi-turn and be thermally cured.That is,
From lower floor (inner side) towards the stepped construction of one group of prepreg 1X (simultaneously wound multilayer 95) in upper strata (outside) and from upper strata
(outside) is mutually the same towards one group of prepreg 1Y (simultaneously wound multilayer 96) of lower floor (inner side).
It is as shown in figure 16 by the plain weave impregnated of thermosetting resin piece in the middle of each embodiment of the embodiment above
Plain weave fabric made by fabric (biaxial braid fabric) prepreg 2C not can serve as torsional rigidity and keep prepreg 2, and not
As a pair of biasing prepreg 2A and 2B.In the middle of the embodiment, plain weave fabric prepreg 2C is set, with
So that a pair of fiber yarn 2C-1 and 2C-2 are symmetrically handed over relative to cylinder axis direction with symmetry angle (for example, ± 45 degree)
Fork.
Additionally, the three axle braided fabrics by made by the three axle braided fabrics impregnated of thermosetting resin piece as shown in figure 17 are pre-
Leaching material base 2D can serve as torsional rigidity and keep prepreg 2.In the middle of the embodiment, to three axle braided fabric prepreg
2D is set so that weft yarn 2D-1 is parallel to cylinder axis direction, and cause a pair of warp thread 2D-2 and 2D-3 relative to
Cylinder axis direction is symmetrically intersected with symmetry angle (for example, ± 60 degree).On the other hand, as shown in figure 18, can also be to three
Axle braided fabric prepreg 2D is configured, so that weft yarn 2D-1 is orthogonal to cylinder axis direction, and causes a pair of warp thread
2D-2 and 2D-3 is symmetrically intersected relative to cylinder axis direction with symmetry angle (for example, ± 30 degree).
Additionally, the four axle braided fabrics by made by the four axle braided fabrics impregnated of thermosetting resin piece as shown in figure 19 are pre-
Leaching material base 2E can serve as torsional rigidity and keep prepreg 2.In the middle of the embodiment, to four axle braided fabric prepreg
2E is set, so that horizontal yarns 2E-1 are parallel to cylinder axis direction, so as to vertical yarn 2E-2 is orthogonal to Cylindorical rod
Line direction, and a pair of angled yarn 2E-3 and 2E-4 is symmetrical with symmetry angle (such as ± 45 degree) relative to cylinder axis direction
Ground intersects.
It is noted that (the twin shaft volume of the plain weave fabric by made by the plain weave fabric impregnated of thermosetting resin piece as shown in figure 20
Woven fabric) prepreg 8 can serve as preventing the prepreg 3 of flexing, rather than as hoop prepreg.To plain weave fabric
Prepreg 8 is set so that a pair of fiber yarn 8A and 8B with symmetry angle (0 degree with 90 degree) parallel (orthogonal) in circle
Cylinder axis direction.Additionally, four axle braided fabric prepreg 2E as shown in figure 19 can also be used as preventing the preimpregnation of flexing
Material base 3.
In the case of the reinforcing fiber prepreg with textile structural, the textile structural is, for example, mentioned above
Plain weave fabric prepreg 2C, three axle braided fabric prepreg 2D, four axle braided fabric prepreg 2E or plain weave fabric
Prepreg 8, then wire thickness be desirably less than 6K.If wire thickness becomes too much more than 6K, the thickness of prepreg,
And possibly cannot guarantee uniform fabric property (physical property);Additionally, during manufacture around the winding prepreg of heart axle
The machinability of base may deteriorate.
Practical example
(the first practical example)
In the middle of the first practical example, the present inventor creates the prototype of the FRP cylinders of four types:Type A
To D, FRP cylinders of the invention are compared with the FRP cylinders with traditional structure.Figure 21 is for showing each
The view of the multi-lay winding structure of the FRP cylinders of type, and in figure 21, each Regional Representative one surrounded by thick frame
FRP layers.
The FRP cylinders of the structure for each corresponding to that there is the 3rd embodiment of type A and B;In the middle of type A, lead to
Cross at the same the multi-lay winding that carries out and multiple separate sheets are clipped in the middle, and in the middle of type B, without separate sheet by entering simultaneously
Capable multi-lay winding and be caught in the middle.The each of type A and B has two simultaneously wound multilayers, and they are by two-layer
Prepreg is assembled to put and formed, and every group of prepreg is pre- by a pair of biasings being sequentially laminated towards outermost layer side from innermost layer side
(90 degree) of leaching material base (± 45 degree) and hoop prepreg are constituted, and every group of prepreg continuous winding three is enclosed (nine laminations)
And be thermally cured (18 laminations altogether).In figure 21, this two groups of prepreg are shown as shadow region.Internal diameter φ is
33.5mm, external diameter Φ are 38.7mm, and length L is 330.2mm, and the weight of Manufactured FRP cylinders is about 150g.
The FRP cylinders with traditional basic structure that each correspond to of Type C and D (are not while the multilayer for carrying out
Winding type).Type C has three layers of group being alternately arranged, per group by being laminated towards outermost layer side from innermost layer side
FRP layers and another FRP layer are constituted, wherein a pair of biasings that previous FRP layers are only wound up as cylinder by the circle of winding two are pre-
Leaching material base (± 45 degree) is made (four laminations), and wherein latter FRP layer is only wound up as cylinder by the circle of winding two
Ring prepreg (90 degree) is made (two laminations) (18 laminations altogether).Type D has from innermost layer side towards most
The FRP layers and the FRP layers of two Second Types of two first kind of outside side stacking, the wherein FRP of each first kind
A pair of biasings prepreg (± 45 degree) that layer is only wound up as cylinder by the circle of winding three make (six laminations), and wherein
The FRP layers of each Second Type are only wound up as the hoop prepreg (90 degree) of cylinder by the circle of winding three and make that (three folded
Layer) (18 laminations altogether).
The present inventor has carried out moment of torsion destructive test in the prototype of A to the D types of FRP cylinders, and
Confirm that the FRP cylinders (type A and B) manufactured according to the present invention have superiority in torsional strength.For each type of
FRP cylinders perform moment of torsion destructive test twice.
The executive mode of moment of torsion destructive test will be discussed below.Each test block is loaded onto hydraulic torque fracture
In the middle of test equipment, one end is securely locked, by the sine wave with ± 45 degree of amplitudes under 0.02Hz speed come to
Give other end angular displacement.Torsional strength is measured by the moment of torsion detector installed in secure lock end.By being fixed to displacement
The decoder of the axle on end is measuring torsion angle.
Table 1 below shows the moment of torsion destructive test result of the prototype of A to the D types of FRP cylinders.Type A and B are roots
Configured according to the present invention, the type A and B have the torsional strength higher than traditional type C and D, and mean height reaches
100Nm, this demonstrate that the superiority of the multi-lay winding carried out while the present invention.When type A mutually compares with type B
Wait, type A has the torsional strength higher than type B, mean height reaches 180Nm, this demonstrate that the superiority that separate sheet winds.
Table 1
Additionally, when type A mutually compares with type B, the surface configuration of type A than type B surface configuration more
It is smooth, and from the point of view of the outward appearance of type A and B, it is obvious that the formability between them has differences.Additionally, from polishing
In the internal state of type A afterwards and the comparison of the internal state of type B type A is can be seen that with more uniform than type B
Internal structure, which demonstrate separate sheet winding superiority.
(the second practical example)
In the middle of the second practical example, the present inventor creates the prototype of the FRP cylinders of three types:Type E,
F and G.Figure 22 is the view for showing the multi-lay winding structure of the FRP cylinders of each type, and in fig. 22, by thick side
One FRP layer of each Regional Representative that frame is surrounded.
Type E corresponding to the structure with the 4th embodiment FRP cylinders (Figure 11), and with simultaneously wound many
Layer, it is formed by the configuration of one group of prepreg, and one group of prepreg towards outermost layer side from innermost layer side by being sequentially laminated
0 degree of prepreg, (90 degree) of a pair of biasings prepreg (± 45 degree) and hoop prepreg constitute, and one group of preimpregnation
Material base continuous winding five is enclosed and is thermally cured (20 laminations altogether).
Type F corresponding to the structure with the 5th embodiment FRP cylinders (Figure 13), and with simultaneously wound many
Layer, it is formed by the configuration of one group of prepreg, and one group of prepreg towards outermost layer side from innermost layer side by being sequentially laminated
Biasing prepreg (+45 degree), 0 degree prepreg, biasing prepreg (- 45 spend) and hoop prepreg (90 degree) structure
Into, and one group of prepreg continuous winding five encloses and is thermally cured (20 laminations altogether).
Type G is corresponding to the FPR cylinders (being not the multi-lay winding type while carrying out) with traditional basic structure.
Type G be by 0 degree of prepreg two laminations, a pair of biasing prepreg (± 45 degree) two laminations (four laminations),
Two laminations of hoop prepreg (90 degree), three laminations of 0 degree of prepreg, a pair of biasings prepreg (± 45 degree)
Three laminations (20 laminations altogether) of three laminations (six laminations) and hoop prepreg (90 degree) are constituted.
The present inventor has carried out moment of torsion destructive test for the FRP cylinders prototype of type E, F and G, and
Confirm that the FRP cylinders (type E and F) produced according to the present invention have superiority in torsional strength and torsional rigidity.
The torsional fracture test is performed in the way of similar to the first practical example.
Table 2 below shows the moment of torsion destructive test result of the prototype of E, F and G type of FRP cylinders.It is traditional with having
Type G of structure compares, type E configured according to the present invention present be higher by 90Nm higher torsional strength and
It is higher by 20Nm2Higher torsional rigidity.Although the intensity that type E and G are calculated according to CLT (Classical lamination theory) is mutual
It is mutually identical, but type E shows the torsional rigidity of higher torsional strength and Geng Gao than type G, so as to confirm while entering
The superiority of capable multi-lay winding.Additionally, the type F ratio configured according to the present invention has the torsion of type G of traditional structure
Rigidity will low 10Nm2;However, type F presents the higher torsional strength that 120Nm is higher by than type G.
Table 2
(the 3rd practical example)
In the middle of the 3rd practical example, the present inventor creates the prototype of two kinds of FRP cylinders:Type
H and I.Figure 23 is the view for showing the multi-lay winding structure of the FRP cylinders of each type, and in fig 23, by thick side
One FRP layer of each Regional Representative that frame is surrounded.
Type H corresponding to the structure with the 4th embodiment FRP cylinders (Fig. 9), and with simultaneously wound many
Layer, it is formed by the configuration of one group of prepreg, and one group of prepreg towards outermost layer side from innermost layer side by being sequentially laminated
0 degree of prepreg, (90 degree) of a pair of biasings prepreg (± 45 degree) and hoop prepreg constitute, and one group of preimpregnation
Material base continuous winding three is enclosed and is thermally cured (12 laminations altogether).
Type I is corresponding to the FPR cylinders (being not the multi-lay winding type while carrying out) with traditional basic structure.
Type I be by 0 degree of prepreg three laminations, a pair of biasing prepreg (± 45 degree) three laminations (six laminations) and
Three laminations (12 laminations altogether) of hoop prepreg (90 degree) are constituted.
The present inventor has carried out bend fracture test, and channel syndrome for the FRP cylinders prototype of type H and I
The real FRP cylinders (type H) produced according to the present invention have superiority in bending strength and bending stiffness.
Destructive test is curved using the tensioning and compression general purpose test equipment that are equipped with 4 crooked test fixtures,
Its test mode will be discussed below.The cylinder test block of 700mm length is manufactured, and bending has been performed on the cylinder test block
Destructive test, its loading velocity is 5mm per minute, and the distance between the strong point is 600mm, and the distance of interaction load(ing) point is
200mm.Length is loaded into the immediately below of each strong point for the metal core wire of 20mm, its object is to prevent cross-sectional deformation.
Strain gauge is arranged on test block, and the bending strength and bending stiffness of the test block is from the dynamometry for being installed on crosshead
What the measured torsional deformation of sensor determined with load.
Table 3 below shows the bend fracture result of the test of type H of FRP cylinders and I prototypes.With with traditional structure
Type I compare, present to be higher by according to type H of present invention configuration and the higher bending strength of 3.55kNm and be higher by
0.77KNm2Higher bending stiffness.Have been proven that by this way, include that bending is firm by causing one group of prepreg
It is strong that degree keeps prepreg (including that bending stiffness keeps prepreg by causing simultaneously wound multilayer) to also improve bending
Degree and bending stiffness.
Table 3
Prototype | The measured value (kNm) of bending strength | Measured value (the KNm of bending stiffness2) |
Type H | 11.14 | 3.44 |
Type I | 7.59 | 2.67 |
Industrial applicability
FRP cylinders of the invention can be widely applied for various industrial circles, for example, for the power transmission shaft of vehicle,
Drive shaft, stabiliser bar or anti-roll lever.
The description of reference
1st, 1 ', 1 ", 1X, 1Y, 4 one groups of prepreg
2nd, 5 torsional rigidities keep prepreg
A pair of biasing prepreg of 2A, 2B, 5A, 5B
2C is used as the plain weave fabric prepreg that torsional rigidity keeps prepreg
2D is used as the three axle braided fabric prepreg that torsional rigidity keeps prepreg
2E is used as four axles that torsional rigidity keeps prepreg or prevents the prepreg of flexing
Braided fabric prepreg
3rd, 6 the prepreg of flexing is prevented
7 prepreg for preventing explosion
The 8 plain weave fabric prepreg as the prepreg for preventing flexing
9 are used as 0 degree of prepreg that bending stiffness keeps prepreg
10th, 40,70,90,95,96 simultaneously wound multilayer
20th, 50 torsional rigidity retaining layer
A pair of bias layers of 20A, 20B, 50A, 50B
30th, 60 the layer that bursts is prevented
80 bending stiffness retaining layers
100 FRP cylinders
Shaft-like (column) heart axles of M
P1, P2 separate sheet
Claims (13)
1. a kind of method of manufacture FRP cylinders, wherein multiple prepreg are wound up as into cylinder and heat cure is carried out, it is many to be formed
Individual FRP layers, by the way that reinforcing fiber is formed impregnated of thermosetting resin piece, methods described includes the prepreg:
The multi-lay winding process for carrying out simultaneously, wherein when the plurality of prepreg is wound up as cylinder, torsional rigidity is protected
Hold prepreg and prevent the prepreg of flexing to be continuously wound multi-turn while stacking mutually, wherein the torsion
Rigidity keeps prepreg including the fibrage in the cylinder axis direction for favouring the FRP cylinders, and wherein, it is described to prevent
The prepreg of flexing includes being orthogonal to the fibrage in the cylinder axis direction,
It is wherein described while the multi-lay winding process that carries out is performed at least twice, and
To described while the multi-lay winding process for carrying out is performed at least twice wherein on winding direction contrary mutually.
2. the method for manufacture FRP cylinders according to claim 1, wherein, described while the multi-lay winding process for carrying out
In, the torsional rigidity keeps prepreg and the prepreg for preventing flexing by bending stiffness holding prepreg
Multi-turn is continuously wound, the bending stiffness keeps prepreg to include the fibrage parallel to the cylinder axis direction,
And the bending stiffness keeps prepreg to be further layered in the torsional rigidity keeping prepreg and the flexing that prevents
In prepreg.
3. the method for manufacture FRP cylinders according to claim 1, wherein described while during the multi-lay winding for carrying out
Each in the plurality of prepreg being wound has identical length on the cylinder axis direction, and
Wherein, on the cylinder axis direction, the plurality of prepreg is stacked mutually in the whole length of the FRP cylinders.
4. a kind of FRP cylinders, with multiple prepreg, the prepreg by by reinforcing fiber impregnated of thermosetting resin piece
And formed, and the prepreg is wound up as cylinder and has carried out heat cure, to be formed as multiple FRP layers,
Wherein the plurality of FRP layers include simultaneously wound multilayer, and the multilayer is formed by one group of prepreg configuration, and this group pre-
Leaching material base continuous winding multi-turn is simultaneously thermally cured, wherein one group of prepreg includes that the torsional rigidity of stacking mutually keeps pre-
Leaching material base and the prepreg for preventing flexing, wherein the torsional rigidity keeps prepreg to include favouring the FRP cylinders
Cylinder axis direction fibrage, and the wherein described prepreg for preventing flexing includes being orthogonal to the cylinder axis side
To fibrage,
Wherein the plurality of FRP layers include multilayer simultaneously wound described at least two, and
At least two groups prepreg for wherein forming the simultaneously wound multilayer respectively are handed over winding direction contrary mutually
For winding.
5. FRP cylinders according to claim 4, wherein the torsional rigidity keeps prepreg to include a pair of biasing preimpregnation
Material base, the filament fiber direction of the biasing prepreg is with ± α degree (0<α<90) angle and favour the cylinder axis side
To, and
Wherein described to prevent the prepreg of flexing from including hoop prepreg, the filament fiber direction of the hoop prepreg is just
Meet at the cylinder axis direction.
6. FRP cylinders according to claim 5, wherein the filament fiber direction of the pair of biasing prepreg with
± 30 degree, ± 45 degree or ± 60 degree of angle favours the cylinder axis direction.
7. FRP cylinders according to claim 4, wherein one group of prepreg also includes being layered in the torsional rigidity
The bending stiffness in prepreg and the prepreg for preventing flexing is kept to keep prepreg, the bending stiffness to keep
Prepreg has the fibrage parallel to the cylinder axis direction.
8. FRP cylinders according to claim 7, wherein the bending stiffness keeps prepreg to include 0 degree of prepreg,
The filament fiber of 0 degree of prepreg is oriented parallel to the cylinder axis direction.
9. FRP cylinders according to claim 4, wherein the torsional rigidity keeps prepreg to include plain weave fabric preimpregnation
Material base, three axle braided fabric prepreg or four axle braided fabric prepreg,
Wherein described plain weave fabric prepreg is made up of the plain weave fabric impregnated of thermosetting resin piece, and the plain weave fabric is pre-
Leaching material base includes favouring the fibrage in the cylinder axis direction, wherein the three axles braided fabric prepreg by impregnated of
Three axle braided fabrics of thermosetting resin piece are constituted, and the three axles braided fabric prepreg includes favouring the cylinder axis side
To fibrage, and wherein described four axles braided fabric prepreg is by the four axle braided fabric structures impregnated of thermosetting resin piece
Into, and the four axles braided fabric prepreg is including the fibrage for favouring the cylinder axis direction.
10. FRP cylinders according to claim 4, wherein described prevent the prepreg of flexing from presoaking including plain weave fabric
Material base or four axle braided fabric prepreg,
Wherein described plain weave fabric prepreg is made up of the plain weave fabric impregnated of thermosetting resin piece, and the plain weave fabric is pre-
Leaching material base includes being orthogonal to the fibrage in the cylinder axis direction, and wherein described four axles braided fabric prepreg is by soaking
Four axle braided fabrics of stain thermosetting resin piece are constituted, and the four axles braided fabric prepreg includes being orthogonal to the Cylindorical rod
The fibrage in line direction.
11. FRP cylinders according to claim 4, wherein one group of prepreg continuous winding three enclose or more multi-turn and
It is wound up as cylinder.
12. FRP cylinders according to claim 4, wherein the plurality of FRP layers include preventing explosion layer to be used as the FRP
The outermost layer of layer, this prevents explosion layer from being made up of hoop prepreg, and the filament fiber direction of the hoop prepreg is orthogonal to
The cylinder axis direction.
13. FRP cylinders according to claim 4, wherein each prepreg of one group of prepreg is in the circle
There is identical length on cylinder axis direction, and wherein on the cylinder axis direction, the institute of one group of prepreg
State multiple prepreg to be stacked mutually in the whole length of the FRP cylinders.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2009-011142 | 2009-01-21 | ||
JP2009011142 | 2009-01-21 | ||
CN201080005194.4A CN102292208B (en) | 2009-01-21 | 2010-01-14 | Method for producing FRP cylinder and FRP cylinder |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201080005194.4A Division CN102292208B (en) | 2009-01-21 | 2010-01-14 | Method for producing FRP cylinder and FRP cylinder |
Publications (2)
Publication Number | Publication Date |
---|---|
CN104015374A CN104015374A (en) | 2014-09-03 |
CN104015374B true CN104015374B (en) | 2017-04-12 |
Family
ID=42355863
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201080005194.4A Active CN102292208B (en) | 2009-01-21 | 2010-01-14 | Method for producing FRP cylinder and FRP cylinder |
CN201410225187.5A Active CN104015374B (en) | 2009-01-21 | 2010-01-14 | Method for producing frp cylinder and frp cylinder |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201080005194.4A Active CN102292208B (en) | 2009-01-21 | 2010-01-14 | Method for producing FRP cylinder and FRP cylinder |
Country Status (7)
Country | Link |
---|---|
US (1) | US8883060B2 (en) |
EP (1) | EP2390087B1 (en) |
JP (1) | JP5662164B2 (en) |
KR (1) | KR101639067B1 (en) |
CN (2) | CN102292208B (en) |
TW (1) | TWI507329B (en) |
WO (1) | WO2010084809A1 (en) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20100130286A (en) * | 2009-06-03 | 2010-12-13 | 에스케이케미칼주식회사 | Fiber reinforced plastic bolt and method for producing the same |
CN102494009B (en) * | 2011-11-22 | 2014-05-28 | 北京玻钢院复合材料有限公司 | Composite material-made transmission shaft for cooling tower and molding technology thereof |
TWI586893B (en) * | 2011-11-30 | 2017-06-11 | Edwards Japan Ltd | Vacuum pump |
US9273483B2 (en) * | 2012-10-05 | 2016-03-01 | Trident Industries, LLC | Composition fiber glass utility pole |
JP5900385B2 (en) * | 2013-03-12 | 2016-04-06 | 三菱電機株式会社 | Manufacturing method of FRP pipe |
US20140265050A1 (en) * | 2013-03-14 | 2014-09-18 | Bell Helicopter Textron Inc. | Multi-layer and Multi-fiber Orientation Compression Rolling Process |
JP5880671B1 (en) * | 2014-11-28 | 2016-03-09 | 株式会社豊田自動織機 | Shock absorber and method for producing shock absorber |
US20160153080A1 (en) * | 2014-12-01 | 2016-06-02 | Inometa Gmbh & Co. Kg | Method for producing a coated component and a coated component |
CN104632861A (en) * | 2014-12-24 | 2015-05-20 | 芜湖市汽车产业技术研究院有限公司 | Manufacture method of fiber composite material automobile transmission shaft |
JP6553903B2 (en) | 2015-03-19 | 2019-07-31 | 住友理工株式会社 | Manufacturing method of resin molded article |
WO2016202870A1 (en) * | 2015-06-18 | 2016-12-22 | Nuovo Pignone Tecnologie Srl | Casing for a turbomachine |
JP6565410B2 (en) * | 2015-07-21 | 2019-08-28 | 日本精工株式会社 | Rack and pinion steering system |
JP6254564B2 (en) * | 2015-11-18 | 2017-12-27 | トヨタ自動車株式会社 | Tank manufacturing method and tank |
CN105398335A (en) * | 2015-11-27 | 2016-03-16 | 奇瑞汽车股份有限公司 | Composite automotive transmission shaft assembly and manufacturing method thereof |
US10208869B2 (en) * | 2016-12-19 | 2019-02-19 | Peopleflo Manufacturing, Inc. | Multi-piece canister assembly for magnetically coupled fluid handling devices |
JP6614225B2 (en) * | 2017-10-31 | 2019-12-04 | トヨタ自動車株式会社 | Tank manufacturing method and tank |
CN108331257A (en) * | 2018-01-19 | 2018-07-27 | 淮阴工学院 | A kind of FRP pipe concrete coupled columns and preparation method thereof with reinforcing rib |
CN108454078A (en) * | 2018-03-02 | 2018-08-28 | 关清英 | A kind of winding, molding method of fiberglass |
JP6961531B2 (en) * | 2018-05-01 | 2021-11-05 | 藤倉コンポジット株式会社 | FRP cylinder and its manufacturing method |
US20210162686A1 (en) * | 2018-06-07 | 2021-06-03 | Ocv Intellectual Capital, Llc | Systems for and methods of forming structural components |
US11440652B2 (en) * | 2018-08-07 | 2022-09-13 | Textron Innovations Inc. | All-fabric spar for aerodynamic components |
JP7570801B2 (en) * | 2018-09-05 | 2024-10-22 | 三菱ケミカル株式会社 | Golf club shaft and manufacturing method thereof |
US10994512B2 (en) | 2019-03-08 | 2021-05-04 | Goodrich Aerospace Services Private Limited | Hybrid composite tube systems and methods |
EP3888897A4 (en) * | 2019-04-25 | 2022-08-17 | Nitto Boseki Co., Ltd. | Fiber-reinforced resin hollow cylindrical body |
CN111271361A (en) * | 2020-03-23 | 2020-06-12 | 山西佰得拓普工贸有限公司 | Fastening screw for vulcanizing machine, preparation method of fastening screw and vulcanizing machine |
US20240288018A1 (en) * | 2021-06-18 | 2024-08-29 | Toray Industries, Inc. | Joint structure, joint body, and member set |
CN113605605B (en) * | 2021-07-20 | 2024-09-27 | 暨南大学 | FRP rib pipe and manufacturing method thereof |
CN115742486A (en) * | 2022-10-14 | 2023-03-07 | 北京卫星制造厂有限公司 | Grid panel low-density aluminum honeycomb core sandwich structure bending test piece and preparation process thereof |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4571355A (en) * | 1984-11-28 | 1986-02-18 | The Boeing Company | Fiber reinforced resin composites formed of basic ply blankets |
CN101309796A (en) * | 2005-09-16 | 2008-11-19 | 霍尼韦尔国际公司 | Reinforced plastic pipe |
Family Cites Families (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3508677A (en) * | 1968-08-20 | 1970-04-28 | Whittaker Corp | Vessel for storing high-pressure gases |
US3607495A (en) * | 1968-10-22 | 1971-09-21 | Nasa | Tube-fabricating process |
US3775219A (en) * | 1971-04-05 | 1973-11-27 | Goldsworthy Eng Inc | Composite-tape placement head |
US4089190A (en) * | 1976-04-14 | 1978-05-16 | Union Carbide Corporation | Carbon fiber drive shaft |
US4173670A (en) * | 1977-05-27 | 1979-11-06 | Exxon Research & Engineering Co. | Composite tubular elements |
US4172175A (en) * | 1978-02-17 | 1979-10-23 | Tillotson-Pearson, Inc. | Pole construction |
US4171626A (en) * | 1978-03-27 | 1979-10-23 | Celanese Corporation | Carbon fiber reinforced composite drive shaft |
JPH01176478A (en) * | 1987-12-29 | 1989-07-12 | Kawasaki Steel Corp | Applied film thickness control of strips |
CA2026113C (en) * | 1989-01-25 | 1998-12-01 | Tsunoe Igarashi | Prepreg, composite molded body, and method of manufacture of the composite molded body |
JP2593613B2 (en) | 1992-07-06 | 1997-03-26 | 株式会社アマダメトレックス | Spot welding equipment |
JP2553612Y2 (en) * | 1992-08-26 | 1997-11-12 | 藤倉ゴム工業株式会社 | Golf club shaft |
JP3279154B2 (en) * | 1994-12-06 | 2002-04-30 | 東レ株式会社 | Fiber reinforced plastic cylinder |
US5792295A (en) * | 1996-08-12 | 1998-08-11 | Plascore, Inc. | Honeycomb fabrication |
JPH1176478A (en) * | 1997-09-02 | 1999-03-23 | Mizuno Corp | Frp-made shaft |
JP2000245880A (en) * | 1999-03-03 | 2000-09-12 | Fujikura Rubber Ltd | Golf club shaft |
JP3595213B2 (en) | 1999-09-29 | 2004-12-02 | 株式会社東芝 | Method of forming FRP tube |
JP2001205710A (en) * | 2000-01-26 | 2001-07-31 | Daiwa Seiko Inc | Unbonded frp joint structural body |
JP2004121402A (en) * | 2002-09-30 | 2004-04-22 | Mizuno Corp | Golf club shaft |
JP4771209B2 (en) | 2004-07-28 | 2011-09-14 | 東レ株式会社 | FRP cylinder and manufacturing method thereof |
US20060121805A1 (en) * | 2004-12-07 | 2006-06-08 | Krulic Charlie B | Non-woven, uni-directional multi-axial reinforcement fabric and composite article |
JP2006262743A (en) * | 2005-03-23 | 2006-10-05 | Daiwa Seiko Inc | Fishing rod |
JP2007185253A (en) * | 2006-01-11 | 2007-07-26 | Sri Sports Ltd | Golf club shaft |
JP4283846B2 (en) * | 2006-12-14 | 2009-06-24 | Sriスポーツ株式会社 | Golf club shaft and golf club |
US7524248B2 (en) | 2006-09-19 | 2009-04-28 | Sri Sports Limited | Shaft for golf clubs and golf club |
JP4848238B2 (en) * | 2006-09-26 | 2011-12-28 | エムアールシーコンポジットプロダクツ株式会社 | Manufacturing method of fiber reinforced resin tubular body |
JP4842081B2 (en) * | 2006-10-11 | 2011-12-21 | エムアールシーコンポジットプロダクツ株式会社 | Manufacturing method of fiber reinforced resin tubular body |
JP2008271875A (en) * | 2007-04-27 | 2008-11-13 | Daiwa Seiko Inc | Pipe-shaped body |
ITUD20070082A1 (en) * | 2007-05-09 | 2008-11-10 | Italica Spa | PROCEDURE FOR THE PRODUCTION OF SHAFTS FOR SAILBOARDS AND TREE FOR SAILBOARDS OBTAINED THROUGH THIS PROCEDURE |
JP4362788B2 (en) * | 2007-06-12 | 2009-11-11 | Sriスポーツ株式会社 | Manufacturing method of tubular body made of fiber reinforced resin and golf club shaft manufactured by the method |
-
2010
- 2010-01-14 JP JP2010547466A patent/JP5662164B2/en active Active
- 2010-01-14 WO PCT/JP2010/050300 patent/WO2010084809A1/en active Application Filing
- 2010-01-14 US US13/144,778 patent/US8883060B2/en active Active
- 2010-01-14 CN CN201080005194.4A patent/CN102292208B/en active Active
- 2010-01-14 EP EP10733416.1A patent/EP2390087B1/en active Active
- 2010-01-14 KR KR1020117015727A patent/KR101639067B1/en active IP Right Grant
- 2010-01-14 CN CN201410225187.5A patent/CN104015374B/en active Active
- 2010-01-18 TW TW099101180A patent/TWI507329B/en active
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4571355A (en) * | 1984-11-28 | 1986-02-18 | The Boeing Company | Fiber reinforced resin composites formed of basic ply blankets |
CN101309796A (en) * | 2005-09-16 | 2008-11-19 | 霍尼韦尔国际公司 | Reinforced plastic pipe |
Also Published As
Publication number | Publication date |
---|---|
TW201028340A (en) | 2010-08-01 |
TWI507329B (en) | 2015-11-11 |
WO2010084809A1 (en) | 2010-07-29 |
EP2390087A4 (en) | 2016-11-30 |
EP2390087B1 (en) | 2018-03-07 |
KR20110117077A (en) | 2011-10-26 |
JPWO2010084809A1 (en) | 2012-07-19 |
US8883060B2 (en) | 2014-11-11 |
EP2390087A1 (en) | 2011-11-30 |
JP5662164B2 (en) | 2015-01-28 |
CN102292208B (en) | 2014-09-10 |
CN104015374A (en) | 2014-09-03 |
US20110281061A1 (en) | 2011-11-17 |
KR101639067B1 (en) | 2016-07-12 |
CN102292208A (en) | 2011-12-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN104015374B (en) | Method for producing frp cylinder and frp cylinder | |
JPH05505228A (en) | Composite tubular member with axial fibers adjacent sidewalls | |
JP6747984B2 (en) | Torsional loaded rod-like component with various fiber reinforcements for tensile and compressive loading | |
CN107850259A (en) | Strengthen the pressure vessel of end socket | |
JPH06508404A (en) | Asymmetric braid formation of modified fiber reinforced products | |
KR20120139685A (en) | Golf club shaft and golf club using same | |
KR102242337B1 (en) | Apparatus of manufacturing the pressure vessel for storing high pressure gas | |
CN111503265B (en) | High-pressure tank and method for manufacturing high-pressure tank | |
US20180250906A1 (en) | Composite members and methods of manufacturing same | |
WO2017038445A1 (en) | Fiber structure and fiber reinforced composite material | |
BRPI0516229B1 (en) | FLEXIBLE CONDUCT FOR TRANSPORTING HYDROCARBONS | |
EP3966022B1 (en) | Fibre-reinforced composite tubular shafts and method of manufacturing thereof | |
US10828845B2 (en) | Wire material for elastic member and elastic member | |
JP7287162B2 (en) | Fiber structures and fiber reinforced composites | |
JP7040347B2 (en) | Pressure vessel and manufacturing method of pressure vessel | |
WO2017102165A1 (en) | Pressure vessel having continuous fibers | |
JP7066602B2 (en) | Tubular body and method for manufacturing tubular body | |
KR100361546B1 (en) | Method for shaft produce of golf club | |
US20170198421A1 (en) | Method of fabricating a textile structure of varying thickness | |
JP2011212463A (en) | Golf club shaft and golf club using the same | |
WO2012014605A1 (en) | Fiber substrate and fiber-reinforced composite material | |
JPH0790552B2 (en) | Reinforcing tubular preform material | |
WO2015004819A1 (en) | Golf club shaft, golf club using same, and golf club shaft manufacturing method |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |